GB878988A - Improvements in or relating to a turbine or compressor inlet nozzle assembly - Google Patents

Improvements in or relating to a turbine or compressor inlet nozzle assembly

Info

Publication number
GB878988A
GB878988A GB13432/58A GB1343258A GB878988A GB 878988 A GB878988 A GB 878988A GB 13432/58 A GB13432/58 A GB 13432/58A GB 1343258 A GB1343258 A GB 1343258A GB 878988 A GB878988 A GB 878988A
Authority
GB
United Kingdom
Prior art keywords
sectors
vanes
turbine
housing
assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB13432/58A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Publication of GB878988A publication Critical patent/GB878988A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB13432/58A 1957-10-31 1958-04-28 Improvements in or relating to a turbine or compressor inlet nozzle assembly Expired GB878988A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE360074X 1957-10-31

Publications (1)

Publication Number Publication Date
GB878988A true GB878988A (en) 1961-10-04

Family

ID=6291742

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13432/58A Expired GB878988A (en) 1957-10-31 1958-04-28 Improvements in or relating to a turbine or compressor inlet nozzle assembly

Country Status (3)

Country Link
CH (1) CH360074A (fr)
FR (1) FR1195960A (fr)
GB (1) GB878988A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3685921A (en) * 1969-08-14 1972-08-22 Bennes Marrcl Gas turbine with variable blade distributor
EP1143111A3 (fr) * 2000-04-04 2003-05-07 Man B&W Diesel Aktiengesellschaft Turbomachine axiale avec des aubes de guidage variables
US10711798B2 (en) 2016-07-13 2020-07-14 MTU Aero Engines AG Variable turbomachine vane cascade

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1239889B (de) * 1963-06-28 1967-05-03 Licentia Gmbh Eintrittsleitschaufelkranz fuer Axialturbinen, insbesondere Axialgasturbinen, mit radial federnd angedrueckten Ringsegmenten
EP0161559A3 (fr) * 1984-05-15 1987-05-13 A. S. Kongsberg Väpenfabrikk Dispositif régulateur de l'insertion et de l'orientation d'aubes directrices d'admission pour compresseurs
DE4309637A1 (de) * 1993-03-25 1994-09-29 Abb Management Ag Radialdurchströmte Abgasturboladerturbine
DE4309636C2 (de) * 1993-03-25 2001-11-08 Abb Turbo Systems Ag Baden Radialdurchströmte Abgasturboladerturbine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3685921A (en) * 1969-08-14 1972-08-22 Bennes Marrcl Gas turbine with variable blade distributor
EP1143111A3 (fr) * 2000-04-04 2003-05-07 Man B&W Diesel Aktiengesellschaft Turbomachine axiale avec des aubes de guidage variables
KR100824894B1 (ko) * 2000-04-04 2008-04-23 만 디젤 에스이 조절 가능한 일련의 가이드 블레이드를 포함하는 가이드 장치를 갖춘 축류 유체 기계
EP2243932A2 (fr) * 2000-04-04 2010-10-27 MAN Diesel SE Turbomachine axiale avec une tuyère de guidage comprenant un étage d'aubes de guidage variables
EP2243932A3 (fr) * 2000-04-04 2011-01-26 MAN Diesel SE Turbomachine axiale avec une tuyère de guidage comprenant un étage d'aubes de guidage variables
US10711798B2 (en) 2016-07-13 2020-07-14 MTU Aero Engines AG Variable turbomachine vane cascade

Also Published As

Publication number Publication date
FR1195960A (fr) 1959-11-20
CH360074A (de) 1962-02-15

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